About: IIL IS-8

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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The IIL IS-8 was a two-seat sailplane designed by Iosif Șilimon and built in Romania in 1960. They served with Romanian gliding clubs.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188
rdfs:label	IIL IS-8 (en)
rdfs:comment	The IIL IS-8 was a two-seat sailplane designed by Iosif Șilimon and built in Romania in 1960. They served with Romanian gliding clubs. (en)
dcterms:subject	1950s Romanian sailplanes
Wikipage page ID	41647521 (xsd:integer)
Wikipage revision ID	994909688 (xsd:integer)
Link from a Wikipage to another Wikipage	Romania NACA airfoil Monoplane Perspex Elevator (aircraft) Sailplane Shoulder wing Plywood Tandem Trim tab Aileron Fuselage Leading edge Aircraft canopy Aircraft fabric covering Fin Balanced rudder Monocoque Trailing edge Motor glider Iosif Șilimon Aerobatics Chord (aircraft) Landing gear Cockpit 1950s Romanian sailplanes IIL IS-5 IIL IS-7 Air brake (aircraft) Cantilever Dihedral (aircraft) Spar (aviation) dbr:IIl_IS-9
sameAs	IIL IS-8 IIL IS-8 IIL IS-8
sink rate ms	0.980000 (xsd:double)
sink rate note	minimum, at (en)
span m	13.350000 (xsd:double)
stall speed kmh	62 (xsd:integer)
wing area sqm	15.450000 (xsd:double)
wing loading kg/m	25.800000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Iosif_Silimon_aircraft
dbp:primeUnits%3F_	met (en)
first flight	1960-09-14 (xsd:date)
national origin	Romania
crew	Two (en)
designer	Iosif Șilimon
manufacturer	Intreprinderea de industrie Locală (en)
ref	The World's Sailplanes , pp. 198–9 (en)
type	Two seat sailplane (en)
has abstract	The IIL IS-8 was a two-seat sailplane designed by Iosif Șilimon and built in Romania in 1960. They served with Romanian gliding clubs. (en)
airfoil	NACA airfoil
aspect ratio	11.500000 (xsd:double)
empty weight kg	220 (xsd:integer)
empty weight note	equipped (en)
glide ratio	best, 23:1 at (en)
gross weight kg	400 (xsd:integer)
length m	7.350000 (xsd:double)
never exceed speed kmh	180 (xsd:integer)
never exceed speed note	placard, smooth air Rough air speed max: Aerotow speed: *Winch launch speed: (en)
gold:hypernym	Sailplane
prov:wasDerivedFrom	wikipedia-en:IIL_IS-8?oldid=994909688&ns=0
page length (characters) of wiki page	6763 (xsd:nonNegativeInteger)
designer	Iosif Șilimon
origin	Romania
type	Sailplane
foaf:isPrimaryTopicOf	wikipedia-en:IIL_IS-8
is Link from a Wikipage to another Wikipage of	List of aircraft (I) Industria Aeronautică Română List of gliders (I) List of Romanian gliders Iosif Șilimon IIL IS-7 IIL IS-9
is foaf:primaryTopic of	wikipedia-en:IIL_IS-8

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